Self-lubricating conductive bearing
US-2020392991-A1 · Dec 17, 2020 · US
US11293495B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11293495-B2 |
| Application number | US-202016898878-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 11, 2020 |
| Priority date | Jun 14, 2019 |
| Publication date | Apr 5, 2022 |
| Grant date | Apr 5, 2022 |
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A bush assembly configured to be disposed between a first component and a second component movably coupled to the first component, the bush assembly comprising a first bush portion comprising a self-lubricating material; and a second bush portion, the second bush portion having greater electrical conductivity than the first bush portion, wherein the second bush portion provides a conductive path between the first component and the second component.
Opening claim text (preview).
The invention claimed is: 1. A bush assembly configured to be disposed between a first component and a second component movably coupled to the first component, the bush assembly comprising: a first bush portion comprising a self-lubricating material; and a second bush portion, the second bush portion having greater electrical conductivity than the first bush portion, wherein the second bush portion provides a conductive path between the first component and the second component, and the second bush portion is removable from the first bush portion, and wherein a cross-sectional shape of the second bush provides for elastic deformation. 2. The bush assembly according to claim 1 , wherein the second bush portion comprises any of an electrically conductive elastomer, graphite, or a metallic material. 3. The bush assembly according to claim 1 , further comprising a third bush portion comprising the self-lubricating material, wherein the second bush portion is located between the first bush portion and third bush portion. 4. The bush assembly according to claim 3 , wherein the second bush portion is configured to exert a force on at least one of the first bush portion and the third bush portion. 5. The bush assembly according to claim 1 further comprising at least one flange attached to at least one of the first bush portion and the second bush portion. 6. The bush assembly according to claim 1 , wherein the second bush portion is configured to exert a force on at least one of the first component and the second component. 7. The bush assembly according to claim 6 , wherein the second bush portion is assembled in the bush assembly in a compressed state to thereby generate the force. 8. The bush assembly according to claim 1 , wherein the first bush portion and the second bush portion each has a respective inner surface in contact with the first component, and a respective outer surface in contact with the second component. 9. A joint assembly comprising: a first component; a second component movably coupled to the first component; and a bush assembly disposed between the first component and the second component, the bush assembly comprising: a first bush portion comprising a self-lubricating material; and a second bush portion, the second bush portion having greater electrical conductivity than the first bush portion, wherein the second bush portion provides a conductive path between the first component and the second component, the second bush portion is removable from the first bush portion, and wherein a cross-sectional shape of the second bush provides for elastic deformation. 10. The joint assembly according to claim 9 , wherein the first component is a joint pin and the second component is pivotally coupled to the joint pin. 11. The joint assembly according to claim 9 , wherein the first component is a shaft, the shaft being coupled to the second component so that the shaft can move relative to the second component along a longitudinal axis of the shaft. 12. An aircraft landing gear assembly comprising one or more joint assemblies according to claim 9 . 13. An aircraft comprising one or more aircraft landing gear assemblies according to claim 12 .
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